发明名称 |
METHOD OF STARTING SOLID-PROPELLANT ROCKET ENGINE |
摘要 |
FIELD: war materiel; solid-propellant rocket engines. ^ SUBSTANCE: proposed method of starting solid-propellant rocket engine comes to following: firstly, igniter is set into action and then combustion products of igniter act onto solid-propellant charge to open nozzle cover. Igniter operates both at moment of opening of nozzle cover and after opening, until engine comes to nominal rating conditions. Nozzle cover is opened at pressure in combustion chamber not lower than stable burning pressure of proposed solid-propellant charge. These conditions are maintained after opening of nozzle cover until engine comes to nominal rating conditions. ^ EFFECT: improved reliability of starting of solid-propellant rocket engine at extreme below-zero temperatures. ^ 3 cl |
申请公布号 |
RU2308609(C1) |
申请公布日期 |
2007.10.20 |
申请号 |
RU20050141003 |
申请日期 |
2005.12.27 |
申请人 |
GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA" |
发明人 |
STEPANICHEV IGOR' VENIAMINOVICH;ZAMARAKHIN VASILIJ ANATOL'EVICH;MIRONOV JURIJ IVANOVICH;KOLOTILIN VLADIMIR IVANOVICH;SHIGIN ALEKSANDR VIKTOROVICH;KOSIN MIKHAIL EVGEN'EVICH |
分类号 |
F02K9/95 |
主分类号 |
F02K9/95 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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